CAJ | 학술논문

　　针对飞机制动用碳刹车材料力矩冲锋、系数波动较大等对系统的影响，本文从峰谷比η、冲峰时间TC、平均力矩MA等碳盘参数入手，采用初始加压IPP、刹车指令多级处理技术MPTB、五级偏压调节PPB等技术，重点以控制角度提高系统对碳盘的适应性，动力联试表明：相对传统刹车模式，新方法对不同厂家、不同工艺的刹车盘适应性更强、制动过程更加平稳。这对提高现役飞机制动的安全性和可靠性具有重要现实意义。
　　침대비궤제동용탄찰차재료력구충봉、계수파동교대등대계통적영향，본문종봉곡비η、충봉시간TC、평균력구MA등탄반삼수입수，채용초시가압IPP、찰차지령다급처리기술MPTB、오급편압조절PPB등기술，중점이공제각도제고계통대탄반적괄응성，동력련시표명：상대전통찰차모식，신방법대불동엄가、불동공예적찰차반괄응성경강、제동과정경가평은。저대제고현역비궤제동적안전성화가고성구유중요현실의의。
Aiming at torque assault and coefficient fluctuation influence aircraft braking system by using carbon brake, the IPP, MTPB and PPB are used to improve the brake material adaptability with the material characteristics, such as peak-to-valley ratio, the pea times T_C and average torque M_A. The angle was controlled to improved carbon brake adaptability. The dynamic inertia tests show that the way increases the adaptability of carbon brakes with different manufacturers and diverse processes and has more stable braking process, relative to the traditional brake mode. That has important practical significance to improve the safety and reliability of aircraft braking system.